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Boron-Based Fuel-Rich Propellant: Properties, Combustion, and Technology Aspects

Editat de WeiQiang Pang
en Limba Engleză Hardback – 29 apr 2019
Boron-Based Fuel-Rich Solid Rocket Propellant Technology is a professional book that systematically introduces the latest research progress for boron-based fuel-rich solid propellants. It covers surface modifications, coating and agglomerating techniques, granulation, and characterization of amorphous boron powders, and its application to fuel-rich solid rocket propellants. Technologies for controlling the processing methods and combustion performance of fuel-rich propellants are examined, and the book concludes with a summary of the research progress in boron-based fuel-rich solid propellants and a look forward to the foreseeable development trends of military applications.
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Specificații

ISBN-13: 9780367141660
ISBN-10: 0367141663
Pagini: 345
Ilustrații: 28 Line drawings, color; 111 Line drawings, black and white; 27 Halftones, color; 50 Halftones, black and white; 120 Tables, black and white; 55 Illustrations, color; 161 Illustrations, black and whit
Dimensiuni: 178 x 254 x 25 mm
Greutate: 1.1 kg
Ediția:1
Editura: CRC Press
Colecția CRC Press

Public țintă

Professional Practice & Development

Cuprins

1. Basic Formulations and Components of Ramjet Propellants 2. Surface Modification and Characterization of Boron Powder 3. The Surface-Interfacial Properties of Boron and Binder System 4. Rheological Properties 5. Energetic Properties 6. Combustion Properties 7. Combustion Performance of Model Propellant with Boron and Boron-Containing Compounds 8. Application Perspectives and Development Trends of Boron-Based Fuel-Rich Propellants

Descriere

Boron powder, with high gravimetric and volumetric heat of combustion, is a promising candidate metal fuels for fuel rich solid propellants, attracting much attention from researchers all over the world. Boron-based Fuel-Rich Solid Rocket Propellant Technology introduces the latest research in the area of boron-based fuel rich solid propellants.